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Numerical simulation of the oxygen-methane mixture combustion products supersonic jet outflow from the low-thrust rocket engine nozzle taking into account variability in their thermal physical properties
| Authors: Taran K.A. | Published: 10.12.2023 |
| Published in issue: #10(87)/2023 | |
| DOI: DOI: 10.18698/2541-8009-2023-10-946 | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: numerical simulation, low-thrust rocket engine, combustion products, oxygen, methane, computational hydraulic gas dynamics, supersonic flow | |